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Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate, Ti-6Al-4V, Stress Relieved
- Aerospace Material Specification
- AMS7004
- Current
Published
2019-01-31
by SAE International in United States
This specification covers preforms fabricated up through 5.5 inches (140 mm) inclusive in deposition width thickness (see 8.2.5) using a Plasma Arc Directed Energy Deposition (PA-DED) additive manufacturing process on a Ti-6Al-4V substrate that are subjected to post-deposition stress relief heat treatment. This is a wire fed additive manufacturing process. If required by the CEO, preforms may require subsequent machining to meet requirements for their intended final part application.
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Wire Fed Plasma Arc Directed Energy Deposition Additive Manufacturing Process
- Aerospace Material Specification
- AMS7005
- Current
Published
2019-01-31
by SAE International in United States
This specification establishes process controls for the repeatable production of preforms by Wire Fed Plasma Arc Directed Energy Deposition (PA-DED). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03La
- Aerospace Material Specification
- AMS7013
- Current
Published
2019-01-03
by SAE International in United States
The intended upper bound of this specification is that the particle size distribution (PSD) of powders supplied shall be <60 mesh (250 µm) and that no powder (0.0 wt.%) greater than 40 mesh (425 µm) is allowed.
Laser Powder Bed Fusion Process
- Aerospace Material Specification
- AMS7003
- Current
Published
2018-06-08
by SAE International in United States
This specification establishes process controls for the repeatable production of aerospace parts by Laser Powder Bed Fusion (L-PBF). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
Process Requirements for Production of Metal Powder Feedstock for Use in Additive Manufacturing of Aerospace Parts
- Aerospace Material Specification
- AMS7002
- Current
Published
2018-06-08
by SAE International in United States
This specification is to prescribe process requirements for production of metal powder feedstock for use in additive manufacturing of aerospace parts.
Laser-Powder Bed Fusion (L-PBF) Produced Parts, Nickel Alloy, Corrosion and Heat-Resistant, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb Stress Relieved, Hot Isostatic Pressed and Solution Annealed
- Aerospace Material Specification
- AMS7000
- Current
Published
2018-06-08
by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of parts produced by laser-powder bed fusion (L-PBF) that are subjected to post-deposition stress relief (SR), hot isostatic press (HIP) and solution anneal operations. Parts may require subsequent machining or surface finishing to meet specific application requirements.
Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb
- Aerospace Material Specification
- AMS7001
- Current
Published
2018-06-08
by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of pre-alloyed powder.
Titanium Alloy Direct Deposited Products 6Al - 4V Annealed
- Aerospace Material Specification
- AMS4999A
- Current
Published
2016-09-26
by SAE International in United States
This specification covers metal products fabricated by direct metal deposition.
Titanium Alloy Laser Deposited Products 6Al - 4V Annealed
- Aerospace Material Specification
- AMS4999
- Historical
Published
2002-02-20
by SAE International in United States
This specification covers metal products fabricated by laser deposition.